CN213387637U - Hoisting frame for assembling aircraft parts - Google Patents
Hoisting frame for assembling aircraft parts Download PDFInfo
- Publication number
- CN213387637U CN213387637U CN202022348360.4U CN202022348360U CN213387637U CN 213387637 U CN213387637 U CN 213387637U CN 202022348360 U CN202022348360 U CN 202022348360U CN 213387637 U CN213387637 U CN 213387637U
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- fixedly connected
- frame
- top end
- motor
- rubber pad
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- 238000001125 extrusion Methods 0.000 claims abstract description 16
- 238000009434 installation Methods 0.000 abstract description 7
- 230000000694 effects Effects 0.000 abstract description 4
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model relates to the technical field of assembly, in particular to a hoisting frame for aircraft part assembly, which comprises a traveling frame, wherein the tail end of a first motor spindle is fixedly connected with a first screw rod, the outer side of the first screw rod is spirally connected with a slide block, the top end of the slide block is fixedly connected with a hydraulic lifting column, the top end of the slide block is fixedly connected with a hollow tube, and the top end of the fixed frame is fixedly connected with a limit block, the utility model adjusts the height of a wing through the hydraulic lifting column, fixes the wing through an electric telescopic rod extrusion plate, improves the fixing effect, lifts the part to a proper position for installation through a traveling crane, enables the rotating shaft to rotate towards two ends through a machine body extrusion plate, enables a slide rod lower frame extrusion spring to be formed by a connecting block, enlarges the space between two support plates, can adjust the space between the support plates again through a, does not need to be replaced, improves the working efficiency, has wide market value and is worth popularizing.
Description
Technical Field
The utility model relates to the field of assembly technology, specifically a hoist and mount frame for aircraft spare part assembly.
Background
The airplane assembly is an important link of airplane manufacturing, the coordination between parts, parts and tools, and between tools is ensured, and further the airplane manufacturing coordination mode for ensuring the assembly accuracy is an important characteristic of airplane manufacturing.
In the process of airplane assembly or maintenance, parts need to be lifted to or from an installation position by using lifting appliance equipment, wings and an airplane body need to be fixed, the airplane body and the wings cannot be directly installed after fixed installation, and the existing airplane body and wing installation platform is complex in structure and poor in flexible adjustment performance.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide the theme to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
a hoisting frame for assembling airplane parts comprises a traveling frame, wherein a bottom plate is fixedly connected to the inner side of the bottom end of the traveling frame, a controller is fixedly connected to the left end of the traveling frame, a first motor is fixedly connected to the left end and the right end of the traveling frame, a first screw is fixedly connected to the tail end of a main shaft of the first motor, a sliding block is spirally connected to the outer side of the first screw, a hydraulic lifting column is fixedly connected to the top end of the sliding block, a hollow tube is fixedly connected to the top end of the sliding block, a fixed table is fixedly connected to the top end of the hydraulic lifting column, a first rotating disc is arranged at the top end of the fixed table, supporting plates are fixedly connected to the front end and the rear end of the first rotating disc, a connecting plate is fixedly connected to the top end of the supporting plates, a second motor is fixedly connected, the utility model discloses a portable high-speed electric scooter, including connecting plate, connecting plate one end fixedly connected with second rubber pad, the equal fixedly connected with electric telescopic handle in both ends around the first carousel, bottom plate top fixedly connected with brace table, the brace table top is provided with the second carousel, second carousel right-hand member fixedly connected with third motor, the terminal fixedly connected with second screw rod of third motor main shaft, second screw rod outside spiral connection has the mount, the inboard fixedly connected with spring of mount, spring top fixedly connected with litter, the litter top is rotated and is connected with the connecting block, connecting block top fixedly connected with layer board, mount top fixedly connected with stopper, fixed station bottom end fixedly connected with traveller, the inboard sliding connection in traveller top has the driving a vehicle.
Preferably, the number of the first motor, the first screw rod, the sliding block, the hydraulic lifting column, the hollow tube, the fixed table and the first rotary table is two, and the number of the supporting plate, the connecting plate, the second motor, the extrusion plate, the first rubber pad, the second rubber pad, the electric telescopic rod and the sliding column is four and is symmetrical to the center of the travelling crane.
Preferably, the supporting plate is rotatably connected with the fixed frame through a rotating shaft.
Preferably, the top end of the fixing frame is provided with an arc-shaped groove, and the top end of the limiting block is provided with an arc-shaped groove.
Preferably, the supporting plate, the connecting plate, the second motor, the extrusion plate, the first rubber pad, the second rubber pad, the electric telescopic rod and the first rotary table are in central symmetry.
Compared with the prior art, the beneficial effects of the utility model are that:
1. in the utility model, through the arrangement of the first turntable, the support plate, the connecting plate, the second motor, the extrusion plate, the first rubber pad, the second rubber pad and the electric telescopic rod, the wing is placed on the first turntable through the crane, the hydraulic lifting column is controlled through the controller, the height of the wing is adjusted, the electric telescopic rod drives the connecting plate to slide in the inner side of the support plate, the second rubber pad extrudes the wing, the extrusion plate and the first rubber pad are driven to rotate through the second motor, the wing is fixed again, the fixing effect is improved, the part of the wing is lifted to a proper position for installation through the crane, the position of the wing is adjusted through the first turntable after the wing is completed, the wing is directly installed through the first screw rod, and the installation efficiency is improved;
2. the utility model discloses in, second carousel through setting up, the third motor, the second screw rod, the mount, a spring, the litter, the connecting block, layer board and stopper, through fuselage extrusion layer board, make the layer board rotate to both ends through the pivot, layer board extrusion connecting block makes litter undercarriage extrusion spring, make the space grow between two layer boards, drive the second screw rod through the third motor and rotate, make two relative reverse movements of mount, can adjust the space between two layer boards once more, can use the fuselage of equidimension not, do not need to change, and the work efficiency is improved.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of the structure at A of FIG. 1 according to the present invention;
FIG. 3 is a schematic view of the structure of FIG. 1 at B according to the present invention;
fig. 4 is a schematic side view of the first turntable according to the present invention.
In the figure: 1-traveling frame, 2-bottom plate, 3-controller, 4-first motor, 5-first screw, 6-sliding block, 7-hydraulic lifting column, 8-hollow tube, 9-fixed table, 10-first rotary table, 11-supporting plate, 12-connecting plate, 13-second motor, 14-extruding plate, 15-first rubber pad, 16-second rubber pad, 17-electric telescopic rod, 18-supporting table, 19-second rotary table, 20-third motor, 21-second screw, 22-fixed frame, 23-spring, 24-slide rod, 25-connecting block, 26-supporting plate, 27-limiting block, 28-slide column and 29-traveling vehicle.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution:
a hoisting frame for assembling airplane parts comprises a traveling frame 1, a bottom plate 2 is fixedly connected to the inner side of the bottom end of the traveling frame 1, a controller 3 is fixedly connected to the left end of the traveling frame 1, a first motor 4 is fixedly connected to the left end and the right end of the traveling frame 1, a first screw 5 is fixedly connected to the end of a main shaft of the first motor 4, a slider 6 is spirally connected to the outer side of the first screw 5, a hydraulic lifting column 7 is fixedly connected to the top end of the slider 6, a hollow tube 8 is fixedly connected to the top end of the slider 6, a fixed table 9 is fixedly connected to the top end of the hydraulic lifting column 7, a first rotating disc 10 is arranged at the top end of the fixed table 9, a support plate 11 is fixedly connected to the front end and the rear end of the first rotating disc 10, a connecting plate 12 is fixedly connected to the top end of the support plate 11, a second motor, connecting plate 12 one end fixedly connected with second rubber pad 16, equal fixedly connected with electric telescopic handle 17 in both ends around first carousel 10, 2 top fixedly connected with brace table 18 of bottom plate, brace table 18 top is provided with second carousel 19, 19 right-hand members fixedly connected with third motor 20 of second carousel, the terminal fixedly connected with second screw rod 21 of the main shaft of third motor 20, second screw rod 21 outside spiral connection has mount 22, the inboard fixedly connected with spring 23 of mount 22, spring 23 top fixedly connected with litter 24, litter 24 top is rotated and is connected with connecting block 25, connecting block 25 top fixedly connected with layer board 26, mount 22 top fixedly connected with stopper 27, fixed station 9 bottom fixedly connected with traveller 28, the inboard sliding connection in traveller 1 top has driving 29.
The number of the first motor 4, the first screw rod 5, the sliding block 6, the hydraulic lifting column 7, the hollow tube 8, the fixed platform 9 and the first rotating disc 10 is two, and the number of the supporting plate 11, the connecting plate 12, the second motor 13, the extrusion plate 14, the first rubber pad 15, the second rubber pad 16, the electric telescopic rod 17 and the sliding column 28 is four, and the four supporting plates are symmetrical to the center of the traveling frame 1, so that two wings of the airplane can be conveniently matched; the supporting plate 26 is rotationally connected with the fixed frame 22 through a rotating shaft to limit the supporting plate 26; the top end of the fixing frame 22 is provided with an arc-shaped groove, and the top end of the limiting block 27 is provided with an arc-shaped groove, so that the supporting plate 26 can be placed on different airplane bodies; the supporting plate 11, the connecting plate 12, the second motor 13, the extrusion plate 14, the first rubber pad 15, the second rubber pad 16, the electric telescopic rod 17 and the first rotating disc 10 are in central symmetry, and the fixing effect is improved.
The working process is as follows: when the utility model is used, the external power supply is firstly used, when in use, the controller 3 controls the hydraulic lifting column 7 to enable the hydraulic lifting column 7 to drive the fixed platform 9 and the first rotary disk 10 to move up and down, at the moment, the sliding column 28 slides in the hollow tube 8 to limit the fixed platform 9, thereby adjusting the height of the first rotary disk 10, then the machine body is placed on the supporting plate 26 through the travelling crane 29, the supporting plate 26 is extruded through the machine body to rotate towards two ends through the rotating shaft, the supporting plate 26 extrudes the connecting block 25 to enable the sliding rod 24 to lower the frame to extrude the spring 23, the space between the two supporting plates 26 is enlarged, the third motor 20 drives the second screw 21 to rotate, so that the two fixed frames 22 relatively move reversely, the space between the two supporting plates 26 can be adjusted again, the machine bodies with different sizes can be used, the replacement is not needed, the working efficiency is improved, and then the wings are placed on, the connecting plate 12 is driven to slide on the inner side of the supporting plate 11 through the electric telescopic rod 17, the second rubber pad 16 extrudes the wing, the second motor 13 drives the extruding plate 14 and the first rubber pad 15 to rotate, the wing is fixed again, the fixing effect is improved, parts of the wing are hung to a proper position through the crane 29 to be installed, the position of the wing is adjusted through the first rotating disc 10 after the wing is completed, the first screw rod 5 is driven to rotate through the first motor 4, the sliding block 6 drives the wing to be directly installed, and the installation efficiency is improved.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. A hoist and mount frame for aircraft parts assembly, includes truss (1), its characterized in that: the inner side of the bottom end of the walking frame (1) is fixedly connected with a bottom plate (2), the left end of the walking frame (1) is fixedly connected with a controller (3), the left end and the right end of the walking frame (1) are fixedly connected with a first motor (4), the tail end of a main shaft of the first motor (4) is fixedly connected with a first screw (5), the outer side of the first screw (5) is spirally connected with a sliding block (6), the top end of the sliding block (6) is fixedly connected with a hydraulic lifting column (7), the top end of the sliding block (6) is fixedly connected with a hollow tube (8), the top end of the hydraulic lifting column (7) is fixedly connected with a fixed table (9), the top end of the fixed table (9) is provided with a first rotary table (10), the front end and the rear end of the first rotary table (10) are fixedly connected with supporting plates (11), the top end of the supporting plates (11), the main shaft of the second motor (13) is fixedly connected with an extrusion plate (14), the bottom of the extrusion plate (14) is fixedly connected with a first rubber pad (15), one end of the connecting plate (12) is fixedly connected with a second rubber pad (16), the front end and the rear end of the first turntable (10) are both fixedly connected with electric telescopic rods (17), the top end of the bottom plate (2) is fixedly connected with a supporting table (18), the top end of the supporting table (18) is provided with a second turntable (19), the right end of the second turntable (19) is fixedly connected with a third motor (20), the tail end of the main shaft of the third motor (20) is fixedly connected with a second screw rod (21), the outer side of the second screw rod (21) is spirally connected with a fixing frame (22), the inner side of the fixing frame (22) is fixedly connected with a spring (23), the top end of the spring (23) is fixedly connected with, connecting block (25) top fixedly connected with layer board (26), mount (22) top fixedly connected with stopper (27), fixed station (9) bottom fixedly connected with traveller (28), the inboard sliding connection in travelling crane (29) in travelling crane (1) top.
2. A lifting frame for the assembly of aircraft components according to claim 1, characterized in that: the number of the first motor (4), the first screw rod (5), the sliding block (6), the hydraulic lifting column (7), the hollow pipe (8), the fixed table (9) and the first rotary table (10) is two, and the number of the supporting plate (11), the connecting plate (12), the second motor (13), the extrusion plate (14), the first rubber pad (15), the second rubber pad (16), the electric telescopic rod (17) and the sliding column (28) is four and is symmetrical to the center of the travelling frame (1).
3. A lifting frame for the assembly of aircraft components according to claim 1, characterized in that: the supporting plate (26) is rotationally connected with the fixed frame (22) through a rotating shaft.
4. A lifting frame for the assembly of aircraft components according to claim 1, characterized in that: the top end of the fixing frame (22) is provided with an arc-shaped groove, and the top end of the limiting block (27) is provided with an arc-shaped groove.
5. A lifting frame for the assembly of aircraft components according to claim 1, characterized in that: the supporting plate (11), the connecting plate (12), the second motor (13), the extrusion plate (14), the first rubber pad (15), the second rubber pad (16) and the electric telescopic rod (17) are in central symmetry with the first rotary table (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022348360.4U CN213387637U (en) | 2020-10-21 | 2020-10-21 | Hoisting frame for assembling aircraft parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022348360.4U CN213387637U (en) | 2020-10-21 | 2020-10-21 | Hoisting frame for assembling aircraft parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213387637U true CN213387637U (en) | 2021-06-08 |
Family
ID=76189365
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022348360.4U Expired - Fee Related CN213387637U (en) | 2020-10-21 | 2020-10-21 | Hoisting frame for assembling aircraft parts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213387637U (en) |
-
2020
- 2020-10-21 CN CN202022348360.4U patent/CN213387637U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210608 |